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Guidance Performance Analysis of Anti-armor Missile Radar Seeker

He Jun

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Abstract

The technical scheme for anti-armor missile radar seeker is analysed.Based on the analysis of the target characteristics,the signal type and the specific form of high-resolution signal for seeker are expounded.The work mode and work process are designed when seeker is in the ground segment and air segment.The measurement accuracy of the seeker is simulated.The result shows that the ranging accuracy of radar seeker is less than 1 meter and the angular rate error is less than 0.2°/s.With the distance decreasing,the precision is improved progressively.The seeker has high guidance performance and can be realized by present technology.The work in this paper has a certain reference value for the engineering application of anti-armor missile radar seekers.

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What this paper is about

The technical scheme for anti-armor missile radar seeker is analysed.Based on the analysis of the target characteristics,the signal type and the specific form of high-resolution signal for seeker are expounded.The work mode and work process are designed when seeker is in the ground segment and air segment.The measurement accuracy of the seeker is simulated.The result shows that the ranging accuracy of radar seeker is less than 1 meter and the angular rate error is less than 0.2°/s.With the distance decreasing,the precision is improved progressively.The seeker has high guidance performance and can be realized by present technology.The work in this paper has a certain reference value for the engineering application of anti-armor missile radar seekers.

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Available abstract

The technical scheme for anti-armor missile radar seeker is analysed.Based on the analysis of the target characteristics,the signal type and the specific form of high-resolution signal for seeker are expounded.The work mode and work process are designed when seeker is in the ground segment and air segment.The measurement accuracy of the seeker is simulated.The result shows that the ranging accuracy of radar seeker is less than 1 meter and the angular rate error is less than 0.2°/s.With the distance decreasing,the precision is improved progressively.The seeker has high guidance performance and can be realized by present technology.The work in this paper has a certain reference value for the engineering application of anti-armor missile radar seekers.

Key concepts: Radar, Missile, Missile guidance, Process (computing), Radar lock-on, Ranging, Engineering, Secondary surveillance radar

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